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==SUMMARY==
==SUMMARY==
 
i TECHRI'DUICYCLl4 9412050199 941123 PDR ADOCK 05000254 P
i TECHRI'DUICYCLl4 9412050199 941123 PDR   ADOCK 05000254 P                 PDR
PDR


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TABLE OF CONTENTS TEST NO.       TITLE         PAGE 1     SHUTDOWN MARGIN     1 2     CORE VERIFICATION   1 3     INITIAL CRITICAL     2 4     TIP REPRODUCIBILITY 3 AND CORE POWER i
TABLE OF CONTENTS TEST NO.
TECINtirr\U1CYCLl4                                 j i
TITLE PAGE 1
SHUTDOWN MARGIN 1
2 CORE VERIFICATION 1
3 INITIAL CRITICAL 2
4 TIP REPRODUCIBILITY 3
AND CORE POWER i
TECINtirr\\U1CYCLl4 j
i


e                                                                                                     '
e 1.
: 1.         Shutdown Marain Demonstration and Control Rod Functional Checks                 ,
Shutdown Marain Demonstration and Control Rod Functional Checks Purpose The purpose of this test is to demonstrate for this core loading in the most-reactive. condition during the-operating cycle, that
Purpose The purpose of this test is to demonstrate for this core loading in the most-reactive. condition during the-operating cycle, that
- the reactor can be made subcritical with the strongest control rod fully withdrawn and all other rods fully inserted.
                      - the reactor can be made subcritical with the strongest control rod fully withdrawn and all other rods fully inserted.
Criteria If a shutdown margin of 0.290% ok (0.25% + R + B.C settling penalty) cannot be demonstrated with the strongest control rod fully withdrawn, the core loading must be altered to achieve this margin.
Criteria If a shutdown margin of 0.290% ok (0.25% + R + B.C settling penalty) cannot be demonstrated with the strongest control rod                   ;
The core reactivity has been calculated to be at a maximum 0 MWD /ST into the cycle and R is given as 0.0Xok.
fully withdrawn, the core loading must be altered to achieve this margin. The core reactivity has been calculated to be at a maximum 0 MWD /ST into the cycle and R is given as 0.0Xok.
The control rod B,C settling penalty for Unit One is 0.04%ok.
The control rod B,C settling penalty for Unit One is 0.04%ok.
Results and Discussion                                                           ,
Results and Discussion s
s On July 8,1994 control rod E-5 was fully withdrawn to demonstrate                 ,
On July 8,1994 control rod E-5 was fully withdrawn to demonstrate that the reactor would remain subcritical with the strongest rod out. This rod was calculated by Nuclear Fuel Services (NFS) to t
that the reactor would remain subcritical with the strongest rod                 .
have the highest worth with the core fully loaded. The strongest rod out maneuver was performed to allow single control rod withdrawals for CRD testing.
out. This rod was calculated by Nuclear Fuel Services (NFS) to                   t have the highest worth with the core fully loaded. The strongest                 ;
Control rod functional subcritical checks were performed as part of control rod friction testing.
rod out maneuver was performed to allow single control rod withdrawals for CRD testing.
No unexpected reactivity insertions were observed when any of the 177 control rods were withdrawn.
Control rod functional subcritical checks were performed as part                 ;
of control rod friction testing. No unexpected reactivity insertions were observed when any of the 177 control rods were withdrawn.
Prior to the initial critical, NFS calculated the shutdown margin to be 1.22% ok (using a critical eigenvalue of 1.004) at 0 mwd /ST, which is the point of minimum shutdown margin for the cycle (R=0).
Prior to the initial critical, NFS calculated the shutdown margin to be 1.22% ok (using a critical eigenvalue of 1.004) at 0 mwd /ST, which is the point of minimum shutdown margin for the cycle (R=0).
The difference between the estimated and actual critical eigenvalue was 0.494% ok. Corrections for temperature and period were -0.15% ok and .047% ok, respectively. Adding these                           ;
The difference between the estimated and actual critical eigenvalue was 0.494% ok.
corrections to the NFS calculated value, the shutdown margin for                 ,
Corrections for temperature and period were -0.15% ok and.047% ok, respectively. Adding these corrections to the NFS calculated value, the shutdown margin for Cycle 14 was determined to be 1.517% ok.
Cycle 14 was determined to be 1.517% ok.
2.
: 2.         Core Verification                                                                 '
Core Verification
                    , Purpose The purpose of the core verification procedure is to verify proper core location and orientation for each fuel assembly.                               1 I
, Purpose The purpose of the core verification procedure is to verify proper core location and orientation for each fuel assembly.
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    .'                                                                                              i f
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Criteria
Criteria
                ~
~
Prior to reactor startup the actual core configuration shall be verified to be ' identical to the planned core configuration.
Prior to reactor startup the actual core configuration shall be verified to be ' identical to the planned core configuration.
Results and Discussion The Unit One Cycle 14 core verification was completed on July 7,           ,
Results and Discussion The Unit One Cycle 14 core verification was completed on July 7, 1994.
1994. Fuel assembly orientation, seating, and serial number were verified for each assembly.                                               .,
Fuel assembly orientation, seating, and serial number were verified for each assembly.
The first inspect' ion was made to verify orientation and seating of assemblies. A second pass was subsequently made to verify bundle -         ,
The first inspect' ion was made to verify orientation and seating of assemblies. A second pass was subsequently made to verify bundle -
serial numbers. The four assemblies in cell location 42-07 were             '
serial numbers. The four assemblies in cell location 42-07 were found not to be properly seated. These assemblies were removed from the core and the fuel support piece at 42-07 was reseated.
found not to be properly seated. These assemblies were removed from the core and the fuel support piece at 42-07 was reseated.
The four assemblies were then placed back into their. proper locations and verified to be located and seated correctly. ' The 7
The four assemblies were then placed back into their. proper               :
Cycle 14 core map is shown in Figure 1.
locations and verified to be located and seated correctly. ' The           7 Cycle 14 core map is shown in Figure 1.
3.
: 3.             Initial Critical Prediction Purpose The purpose of this test is to demonstrate the ability of NFS to           [
Initial Critical Prediction Purpose The purpose of this test is to demonstrate the ability of NFS to
calculate control rod worths and shutdown margin by predicting the       _;
[
in-sequence critical.                                                      .
calculate control rod worths and shutdown margin by predicting the in-sequence critical.
Criteria                                                                   ,
Criteria NFS' prediction for the critical rod pattern must _ agree within 1%.
NFS' prediction for the critical rod pattern must _ agree within 1%.       ,
Ak to the actual critical rod pattern.
Ak to the actual critical rod pattern. A discrepancy greater than       j 1% Ak will be cause for an On-Site Review and investigation by NFS.                                                                       ;
A discrepancy greater than j
Results and Discussion                                                     ;
1% Ak will be cause for an On-Site Review and investigation by NFS.
On August 19, 1994, at 1408 hours the reactor was brought critical with a reactor water temperature at the time of criticality ofl           i 122oF. The difference between the expected critical rod pattern (at 68oF)~and the actual critical rod. pattern was 0.00894 from rod       '
Results and Discussion On August 19, 1994, at 1408 hours the reactor was brought critical with a reactor water temperature at the time of criticality ofl i
i worth tables supplied by NFS. The temperature effect was -0.0015 Ak from NFS supplied corrections. The excess reactivity from the         -i 111 second period was 0.00047 Ak. These reactivities. sum to               1 0.00697 Ak difference (0.697% Ak) between the~ expected critical           i rod pattern'and the actual rod pattern. This is within the 1% Ak-           l criteria of this test, and NFS' ability to predict control rod             t worths is, therefore, successfully demonstrated.
122oF. The difference between the expected critical rod pattern (at 68oF)~and the actual critical rod. pattern was 0.00894 from rod i
                                                                                                      ]
worth tables supplied by NFS. The temperature effect was -0.0015 Ak from NFS supplied corrections. The excess reactivity from the
-i 111 second period was 0.00047 Ak. These reactivities. sum to 1
0.00697 Ak difference (0.697% Ak) between the~ expected critical i
rod pattern'and the actual rod pattern.
This is within the 1% Ak-l criteria of this test, and NFS' ability to predict control rod t
worths is, therefore, successfully demonstrated.
]
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                                                                                              -4 4 '. - -    Core Power Distribution Symmetry Analysis                               '
-4 4 '. -
Purpose                                                                 i The purpose of this test is to determine the magnitude of-               -
Core Power Distribution Symmetry Analysis Purpose i
indicated core power dist'ibution r      asymmetries using data (TIP           i traces and 00-1) collected in conjunction with the CMC update.           !
The purpose of this test is to determine the magnitude of-indicated core power dist'ibution asymmetries using data (TIP r
Criteria A.                   The total TIP uncertainty (including random noise and geometric uncertainties' obtained by averaging the uncertainties for all data sets) must be less than 9%.                               ,
i traces and 00-1) collected in conjunction with the CMC update.
B.                   The gross check of TIP signal symmetry should yield a maximum deviation between symmetrically located pairs of less than 25%.
Criteria A.
Results and Discussion Due to a forced shutdown, this portion of the startup test program       .
The total TIP uncertainty (including random noise and geometric uncertainties' obtained by averaging the uncertainties for all data sets) must be less than 9%.
has not been. completed. A supplement to this report will be             l issued upon completion of the test or in three months, whichever is-earliest.
B.
The gross check of TIP signal symmetry should yield a maximum deviation between symmetrically located pairs of less than 25%.
Results and Discussion Due to a forced shutdown, this portion of the startup test program has not been. completed. A supplement to this report will be l
issued upon completion of the test or in three months, whichever is-earliest.
t i
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TECihRmUICYCL14                           3
TECihRmUICYCL14 3


FIGURE 1 CYCLE 14                                                                                         .
FIGURE 1 CYCLE 14 QUAD CITIES UNIT 1 REACTOR
QUAD CITIES UNIT 1 REACTOR                                                                                           [   ,
[
1     3     5     7     9   11 13 15 17 19 21 23 25 27 29 31 33 35 37 39 41 43 45 47 49 51 53 55 57 59                                                                                 ,
1 3
60                                                             tmn two tmn tune tes             trax   inus   imm tm7 tum                                                       -
5 7
60 58                                                       tum tras4 tm4: tmes inm tmsc tmn tmo                 in2ss imo tuo tuo4                                                           58 56                                     (mn tms)   tuss 2     tnne (mu tmsc tmo imio inns tmn (mn tmn tmst tusi                                                                    tuss twn twie imx                                         56 54                               tuu tusa tus4 tuss tus2 tmn       uso msu vm msso uso vmo nos mus tmn tmso tun trau ims tvan                                                             54 52                         tmso tmv   tvan iniss msor tma moos     um tum mso4 twa (mu us.si tmn mn ms* tmsi ms4o tytm tras two                             tun                           52 50                   tus2 ten     tea 3 tmo msx   im4: m s3 m ai   tmss vain tmo usu uni twsos u2n tmis um mo nun unn trTns tun                             tymn two                     50 48             tuxi tvm   tun   ten   tnm vmo (mu uns       twso4 vmu tmsi uns two imis uns tmn msn (moi u2n tmn um tmso tmis                               tvm   tm): twee             48 43             tmm   tu4o imes msos vm4     vm   uisi twoo2 msai   msie unr vasi vas vmu msor va2n nx3 msn twni uni nun un vmu                               inm   tvan imos               46 44             tmss tues .msn mo4 tmsi       mu   vma) vaso two     msi tmis uin tmi4 twsti vaisi tmn va2n two mso vmss vam (moo vmes vasn twu tun                                         44 42       tras2 tmu   tmso tmu     mse vans twim van twns m st imo           en     teso was     uns   (mss   um   twns   mn   tmu mso4 tmsa v42n   van tnm     imis tun two           42 40 tus two     mm   imo2 msss   was twns van tum7 um tum3         mss 4 twm   uso   twmi twn4     me     tmn umis tmm us2n two vasn twsis         uns nun     tnm2 tnm   tvm tmu     40 38 tmss two   (nni mus una     (neos mes vas4   mn     twns vmu tms: unis tmos msn vms twns                 urn   tme   nxu twm   va2n vmu uma twoon     va274 nun tw     tms4 tuos   38 33 tmn tmas (mas muo tmn ms, imn             um   tmn vaise twas vmu twne was two2 ima vmos (mn                     mn     tem   vmon tm3: unao mm un4       tmu   vassa inns inm4 tm4o   36 34 tuu tmso imu     n3soo msos twics va2m nw   vain tmos una two       em     twas uin mss im3s was twns               um   inni vains vmu uns   twoos van   nuis (ms   tnm3 tmn   34 32 ten im:7 inns     urn   twm unis twm vmu tmn         mso twns van twsss mm tmn tum vain tmp van to mio imio nun twoos van 2 two vm                                   tuis (mso tuui   32 3D teso inm inns msis (mn vans tme vmu twsu mso twn3 msse twm mm tw= twm vans ime msn twns va2m tws2 nxu twm vans tw man     tmu inm tuns     30 28 ten tmn inne vmx ess twei v43is msas wx teos usu tmn um tmn wn vaan two urn tmst uxo ten uans uxn tam 2 twan uno msss   imm imo tra       28 23 tous tuna inns usos twns mu tnm ua3a tm:4 wio twn2 vano imm u2o tmas two vam twna um tuns mn twn: vans (mss vana tmsa nuo       imii tmso   (mx   26 24 tuxi imu tmn mut vams twin vmis vmos v42s2 twas unn twne vars tmn vais nxu twn4 um twm moor tmss vam msas nuo tmrt uno vmir         (mn   in2s2 tun   24 22 tux 4 tms tmn tmo msss vazia twin mss 4 tmas unze twm vms: twns uns imu twns un. ims                               man twno um (mas van twu3 uns nun tmas               inin trace twa   22 j 23       tuns tuus   (mss inni   um   v4x4 twoo ms2e (Mn     um   tMss   uns   tmn m4s vam tma             u2s   tmn mat     (mas van   (M34 uns   vant inm   imis trats ime         20 18             tux 3 twn   van   unas (mse mo   msa2 vasi twar u2si tmas       uns   twers twsis va2n twm       vaan tmsa   uxu nisse usm inns msa ux*     tuoi tmu               18
9 11 13 15 17 19 21 23 25 27 29 31 33 35 37 39 41 43 45 47 49 51 53 55 57 59 60 tmn two tmn tune tes trax inus imm tm7 tum 60 58 tum tras4 tm4:
, 10             tm*   tun   tmo   msn   msos vasa uru   twem unsa van uso       msse uxoo     uxn una       va m van nun     LWan vam   uxx n3soi un34 in N trao2 1923                 16 14             inso two   tun tmu imse vas2 tmi4 ums twue msas imx uns twus (mn vam (nm                             usu tmu           tmn van m ai            (mai inne imas tmso imu                   14 12                   tms4 tme     tvm   imis vm24 mso varu va2n twin       wo     twur   vam   um     tmn vans twin       um mu     mso ums (ms4 ten tmu ten                             12 i 10                         two ten tuos     tmis mso2   inm man   vams imii     van tmn imm una             tms2 vans Exs     tmn msn l
tmes inm tmsc tmn tmo in2ss imo tuo tuo4 58 56 (mn tms) tuss 2 tusi tnne (mu tmsc tmo imio inns tmn (mn tmn tmst tuss twn twie imx 56 54 tuu tusa tus4 tuss tus2 tmn uso msu vm msso uso vmo nos mus tmn tmso tun trau ims tvan 54 52 tmso tmv tvan iniss msor tma moos um tum mso4 twa (mu us.si tmn mn ms*
tms: tues tun lm4                               10 l 8                                imo (msi tus     tuus   tu4u imp   vmso   ums msso um4         nxie uxos     vm ww 1                                                                                                                              tmu teos (mss traos tmis imi                                     8 6                                       two in3n tuns tun tmoo imu tmu tmo tmn tms4 inn 4 tmse imo tniu tveoi tmas 1
tmsi ms4o tytm tras two tun 52 50 tus2 ten tea 3 tmo msx im4:
tym4 tmas                                       6 4                                                         tmp tuo2         tyT2is tv12sl        tvTns tyf22o tvT2s2 lit 2ss tvT2? tvf24s (valo (m42                                                       4 l 2                                                             twa   tuss 4 tmsi   ruxs   inne   twa   tuni   tuus (mos imas                                                                 2 3     5     7     9 1
m s3 m ai tmss vain tmo usu uni twsos u2n tmis um mo nun unn trTns tun tymn two 50 48 tuxi tvm tun ten tnm vmo (mu uns twso4 vmu tmsi uns two imis uns tmn msn (moi u2n tmn um tmso tmis tvm tm):
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twee 48 43 tmm tu4o imes msos vm4 vm uisi twoo2 msai msie unr vasi vas vmu msor va2n nx3 msn twni uni nun un vmu inm tvan imos 46 44 tmss tues.msn mo4 tmsi mu vma) vaso two msi tmis uin tmi4 twsti vaisi tmn va2n two mso vmss vam (moo vmes vasn twu tun 44 42 tras2 tmu tmso tmu mse vans twim van twns m st imo en teso was uns (mss um twns mn tmu mso4 tmsa v42n van tnm imis tun two 42 40 tus two mm imo2 msss was twns van tum7 um tum3 mss 4 twm uso twmi twn4 me tmn umis tmm us2n two vasn twsis uns nun tnm2 tnm tvm tmu 40 38 tmss two (nni mus una (neos mes vas4 mn twns vmu tms:
unis tmos msn vms twns urn tme nxu twm va2n vmu uma twoon va274 nun tw tms4 tuos 38 33 tmn tmas (mas muo tmn ms, imn um tmn vaise twas vmu twne was two2 ima vmos (mn mn tem vmon tm3:
unao mm un4 tmu vassa inns inm4 tm4o 36 34 tuu tmso imu n3soo msos twics va2m nw vain tmos una two em twas uin mss im3s was twns um inni vains vmu uns twoos van nuis (ms tnm3 tmn 34 32 ten im:7 inns urn twm unis twm vmu tmn mso twns van twsss mm tmn tum vain tmp van to mio imio nun twoos van 2 two vm tuis (mso tuui 32 3D teso inm inns msis (mn vans tme vmu twsu mso twn3 msse twm mm tw=
twm vans ime msn twns va2m tws2 nxu twm vans tw man tmu inm tuns 30 28 ten tmn inne vmx ess twei v43is msas wx teos usu tmn um tmn wn vaan two urn tmst uxo ten uans uxn tam 2 twan uno msss imm imo tra 28 23 tous tuna inns usos twns mu tnm ua3a tm:4 wio twn2 vano imm u2o tmas two vam twna um tuns mn twn:
vans (mss vana tmsa nuo imii tmso (mx 26 24 tuxi imu tmn mut vams twin vmis vmos v42s2 twas unn twne vars tmn vais nxu twn4 um twm moor tmss vam msas nuo tmrt uno vmir (mn in2s2 tun 24 22 tux 4 tms tmn tmo msss vazia twin mss 4 tmas unze twm vms:
twns uns imu twns un. ims man twno um (mas van twu3 uns nun tmas inin trace twa 22 23 tuns tuus (mss inni um v4x4 twoo ms2e (Mn um tMss uns tmn m4s vam tma u2s tmn mat (mas van (M34 uns vant inm imis trats ime 20 j
18 tux 3 twn van unas (mse mo msa2 vasi twar u2si tmas uns twers twsis va2n twm vaan tmsa uxu nisse usm inns msa ux*
tuoi tmu 18 10 tm*
tun tmo msn msos vasa uru twem unsa van uso msse uxoo uxn una va m van nun LWan vam uxx n3soi un34 in N trao2 1923 16 14 inso two tun tmu imse vas2 tmi4 ums twue msas imx uns twus (mn vam (nm usu tmu m ai tmn van (mai inne imas tmso imu 14 12 tms4 tme tvm imis vm24 mso varu va2n twin wo twur vam um tmn vans twin um mu mso ums (ms4 ten tmu ten 12 i
10 two ten tuos tmis mso2 inm man vams imii van tmn imm una tms2 vans Exs tmn msn tms:
tues tun lm4 10 l
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two in3n tuns tun tmoo imu tmu tmo tmn tms4 inn 4 tmse imo tniu tveoi tmas tym4 tmas 6
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tmp tuo2 tv12sl tyT2is tvTns tyf22o tvT2s2 lit 2ss tvT2?
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twa tuss 4 tmsi ruxs inne twa tuni tuus (mos imas 2
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Latest revision as of 00:20, 15 December 2024

Quad-Cities Nuclear Power Station Unit One Cycle Fourteen Startup Test Results Summary
ML20078M904
Person / Time
Site: Quad Cities Constellation icon.png
Issue date: 11/23/1994
From:
COMMONWEALTH EDISON CO.
To:
Shared Package
ML20078M880 List:
References
NUDOCS 9412050199
Download: ML20078M904 (6)


Text

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QUAD-CITIES NL'LLEAR POWER STATION UNIT ONE CYCLE FOURTEEN STARTUP TEST RESULTS

SUMMARY

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TABLE OF CONTENTS TEST NO.

TITLE PAGE 1

SHUTDOWN MARGIN 1

2 CORE VERIFICATION 1

3 INITIAL CRITICAL 2

4 TIP REPRODUCIBILITY 3

AND CORE POWER i

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Shutdown Marain Demonstration and Control Rod Functional Checks Purpose The purpose of this test is to demonstrate for this core loading in the most-reactive. condition during the-operating cycle, that

- the reactor can be made subcritical with the strongest control rod fully withdrawn and all other rods fully inserted.

Criteria If a shutdown margin of 0.290% ok (0.25% + R + B.C settling penalty) cannot be demonstrated with the strongest control rod fully withdrawn, the core loading must be altered to achieve this margin.

The core reactivity has been calculated to be at a maximum 0 MWD /ST into the cycle and R is given as 0.0Xok.

The control rod B,C settling penalty for Unit One is 0.04%ok.

Results and Discussion s

On July 8,1994 control rod E-5 was fully withdrawn to demonstrate that the reactor would remain subcritical with the strongest rod out. This rod was calculated by Nuclear Fuel Services (NFS) to t

have the highest worth with the core fully loaded. The strongest rod out maneuver was performed to allow single control rod withdrawals for CRD testing.

Control rod functional subcritical checks were performed as part of control rod friction testing.

No unexpected reactivity insertions were observed when any of the 177 control rods were withdrawn.

Prior to the initial critical, NFS calculated the shutdown margin to be 1.22% ok (using a critical eigenvalue of 1.004) at 0 mwd /ST, which is the point of minimum shutdown margin for the cycle (R=0).

The difference between the estimated and actual critical eigenvalue was 0.494% ok.

Corrections for temperature and period were -0.15% ok and.047% ok, respectively. Adding these corrections to the NFS calculated value, the shutdown margin for Cycle 14 was determined to be 1.517% ok.

2.

Core Verification

, Purpose The purpose of the core verification procedure is to verify proper core location and orientation for each fuel assembly.

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Criteria

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Prior to reactor startup the actual core configuration shall be verified to be ' identical to the planned core configuration.

Results and Discussion The Unit One Cycle 14 core verification was completed on July 7, 1994.

Fuel assembly orientation, seating, and serial number were verified for each assembly.

The first inspect' ion was made to verify orientation and seating of assemblies. A second pass was subsequently made to verify bundle -

serial numbers. The four assemblies in cell location 42-07 were found not to be properly seated. These assemblies were removed from the core and the fuel support piece at 42-07 was reseated.

The four assemblies were then placed back into their. proper locations and verified to be located and seated correctly. ' The 7

Cycle 14 core map is shown in Figure 1.

3.

Initial Critical Prediction Purpose The purpose of this test is to demonstrate the ability of NFS to

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calculate control rod worths and shutdown margin by predicting the in-sequence critical.

Criteria NFS' prediction for the critical rod pattern must _ agree within 1%.

Ak to the actual critical rod pattern.

A discrepancy greater than j

1% Ak will be cause for an On-Site Review and investigation by NFS.

Results and Discussion On August 19, 1994, at 1408 hours0.0163 days <br />0.391 hours <br />0.00233 weeks <br />5.35744e-4 months <br /> the reactor was brought critical with a reactor water temperature at the time of criticality ofl i

122oF. The difference between the expected critical rod pattern (at 68oF)~and the actual critical rod. pattern was 0.00894 from rod i

worth tables supplied by NFS. The temperature effect was -0.0015 Ak from NFS supplied corrections. The excess reactivity from the

-i 111 second period was 0.00047 Ak. These reactivities. sum to 1

0.00697 Ak difference (0.697% Ak) between the~ expected critical i

rod pattern'and the actual rod pattern.

This is within the 1% Ak-l criteria of this test, and NFS' ability to predict control rod t

worths is, therefore, successfully demonstrated.

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Core Power Distribution Symmetry Analysis Purpose i

The purpose of this test is to determine the magnitude of-indicated core power dist'ibution asymmetries using data (TIP r

i traces and 00-1) collected in conjunction with the CMC update.

Criteria A.

The total TIP uncertainty (including random noise and geometric uncertainties' obtained by averaging the uncertainties for all data sets) must be less than 9%.

B.

The gross check of TIP signal symmetry should yield a maximum deviation between symmetrically located pairs of less than 25%.

Results and Discussion Due to a forced shutdown, this portion of the startup test program has not been. completed. A supplement to this report will be l

issued upon completion of the test or in three months, whichever is-earliest.

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FIGURE 1 CYCLE 14 QUAD CITIES UNIT 1 REACTOR

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